LEFT SIDE - FUSELAGE, MAIN ROTOR AND LANDING GEAR
Cabin doors for general condition, and proper operation vents and
door latching and locking mechanism.
Front compartment door hinge pins properly installed and secured.
Left hand static port free from obstruction.
Access, inspection and compartment doors/covers for secure closure.
Landing gear for condition of skid tubes and fairings; abrasion strips
secure.
Forward and rear landing gear dampers for condition, by observing
stance of helicopter. Visually check dampers for leakage. Replace
damper if leakage is obvious or if extension is unusual.
Passenger step secure and free from damage.
Upper canopy clean and free from damage.
Pylon clean and free from damage.
Main rotor hub, pitch housing and swashplate for obvious damage.
Blade pitch links lockwire for security. Visually inspect main rotor
blade damper attach fitting for cracks, wear and corrosion. Damper
for obvious damage and for security. Scissors for any evidence of
damage or deformation of crank or link.
All main rotor blades for scratches, dents, cracks, corrosion, security
and bond separation at root fittings and doublers.
Main rotor blade leading edge abrasion strip bonding for bonding
separation. Any blisters, bubbling or lifting of edge of abrasion strip
indicates a void.
Handling, Servicing & Maint.
Pilot's Flight Manual
Schweizer RSG, LLC.
Model
269D
Helicopter
7-8
Reissued:
16
Jan 2019
Book 3.indd 170
8/4/19 1:25 PM
